System and method for cooled airflow for dermatological applications

ABSTRACT

A system and method of providing a temperature controlled gaseous medium for dermatological applications is described. The gaseous medium may be cooled and applied to an area such as a skin area to provide an analgesic effect thereon. The system and method also include an automated defrost cycle for minimizing the effects of decreased hydraulic diameter due to freezing.

RELATED APPLICATIONS

The present application is a continuation of U.S. patent applicationSer. No. 12/524,592, filed Dec. 22, 2009. U.S. patent application Ser.No. 12/524,592 is a national-stage entry of International PatentApplication No. PCT/US2008/053888. International Patent Application No.PCT/US2008/053888 claims priority to U.S. Provisional Patent ApplicationNo. 60/889,723, filed Feb. 13, 2007. U.S. patent application Ser. No.12/524,592 and U.S. Provisional Patent Application No. 60/889,723 areincorporated herein by reference.

TECHNICAL FIELD

The present invention relates to gas cooling and, more particularly, butnot by way of limitation to methods of and systems for providing cooledgas for dermatological applications.

RELATED ART

Conventional cooling technology typically includes passive coolingsystems, compressor-based systems, and thermoelectric systems. Incertain passive cooling systems, the air to be cooled is circulated overan air-to-air heat exchanger, which includes folded, finned heatexchangers, heat pipes, etc. The heat is then exchanged with the outsideambient air. As the amount of heat to be removed from the areaincreases, the size of the air-to-air heat exchanger increases.Compressor-based systems function by using a refrigerant and the coolingfunction is achieved by the compression and expansion of therefrigerant. Disadvantage of compressor-based systems include unwantednoise and vibration.

Thermoelectric temperature control systems use thermoelectric devicesthat pump heat using the Peltier effect. Typical thermoelectric devicesincorporate a thermoelectric component utilizing electrical current toabsorb heat from one side of the component and dissipate that heat onthe opposite side. Thermal electric temperature control systems usingthermal electric devices are, as described above, capable of bothheating and cooling, low vibration, relatively high Coefficient OfPerformance (ability to remove heat), low noise, and low profile.

It is known that dermal cooling may provide an analgesic effect such asa numbing of the surface of the skin to diminish pain caused by dermalprocedures, such as, for example, laser or light-treatments andinjections. To provide an analgesic effect by cooling a skin area, someapproaches include the use of a cool object. Often the object is a pieceof metal which has been placed first into a cooling medium, for example,a freezer or an ice bath before its use. Once the object has becomesufficiently cold, the object may be removed from the cooling medium andplaced on the skin surface to provide an analgesic effect. Suchapproaches have disadvantages. If these objects are cooled totemperatures below freezing to allow them to maintain temperatures belowambient for longer periods of time, problems may result from improperuse. For example, one problem that may arise when temperatures belowfreezing are applied to a skin area is that cellular damage may occur.

Medical care providers thus recognize the need to provide carefullyselected warmth and/or cooling directly to patients as part of theirtreatment and therapy. For example, anesthetic properties have beenreported using cold therapy for dermatology patients. Several deviceshave been developed that deliver temperature controlled fluids andgasses to achieve various benefits. Typically, these devices have aheating or a cooling element, a pump for causing the air or fluid toflow, and a thermal interface between the patient and the temperaturecontrolled fluid. One traditional way has been heating or coolingblankets directing a conditioned gas toward a covered person through amultiplicity of orifices in one side of the blanket.

Other methods for cooling the temperature of a surface have beendeveloped such as a roller with a cooling substance contained therein.Other pain management devices have used cooling devices that have ahandle and a cooling head, where the handle contains a cooling substanceto cool the head as it contacts a surface.

Both pre-procedure and post-procedure dermal cooling has been utilizedto protect the skin from damage from light sources used during suchprocedures as laser hair removal and skin peeling. Contact coolers thatcool the skin through direct contact therewith have the disadvantage ofnot allowing the laser to operate on the skin while the contact coolerwas contacting the skin. In the past, air coolers were not preciselycontrolled and would provide air at an output of a delivery hose thatwas below freezing temperatures, for example, −10 to −13° C. The usersof such systems had to spatially dispose the output from the skinsurface in order to avoid the deleterious effects of freezing the skin.This added another level of inaccuracy to the system.

BRIEF SUMMARY OF THE INVENTION

One aspect of an illustrative embodiment of the present inventionrelates to gas coolers for dermatological applications. Moreparticularly, one aspect of an illustrative embodiment relates to amethod of and system for cooling a gaseous medium to a specifiedtemperature and making it available for cooling surfaces, such as, forexample, skin surfaces. In various embodiments, the cooled gas or othergaseous or fluidic medium is pumped from a control unit via an insulatedhose. The control unit may increase or decrease the temperature of thecooled gas depending on user inputted settings. In some embodiments, thecontrol unit may monitor the temperature of the gas exiting the controlunit and calculate the temperature of the gas exiting the insulated tubebased on various criteria including, among other things, the pressureand velocity of the gas leaving the control unit and the pressure andtemperature of the environment surrounding the delivery hose.

In various embodiment a method for thermally affecting a gaseous mediumfor dermatological applications is shown, the method including providinga plurality of thermally controlled flow tunnels; creating a pressuredifferential to impart airflow through a plurality of flow tunnels forthermal interaction therewith; actively cooling the plurality of flowtunnels to a temperature below a freezing point of moisture containedwithin the gaseous medium; monitoring a condition relating to theairflow of the gaseous medium flowing through the flow tunnels; andreducing the level of active cooling of at least one of the plurality offlow tunnels in response to a monitored condition indicative of areduction in a hydraulic diameter of at least one of the plurality offlow tunnels.

In various embodiments, a system for providing a cooled gaseous mediumfor dermatological applications is shown, the system including aplurality of flow tunnels having inlets and outlets; an air moveradapted to impart airflow to a gaseous medium through the plurality offlow tunnels; a plurality of thermoelectric coolers thermally coupled tothe plurality of flow tunnels and adapted to actively remove heattherefrom to cool the gaseous medium flowing therethrough; a sensoradapted to monitor at least one indicator relative to the flow of thegaseous medium through the plurality of flow tunnels and send a signalif a hydraulic diameter of at least one of the plurality of flow tunnelsdecreases; and wherein the amount of heat being actively removed by atleast one of the plurality of thermoelectric coolers from at least oneof the plurality of flow tunnels is reduced in response to the signal.

In some embodiments, the control unit cools a gas such as, for example,ambient air by passing it through heat transfer assemblies. The heattransfer assemblies may have flow tunnels comprising a plurality ofmicrotubes running therethrough, the microtubes having a plurality ofmicrochannels formed along inside surfaces thereof for enhancing thetransferring of heat from air passing therealong. The flow tunnels maybe in thermal communication with thermoelectric coolers (TEC). In someembodiments, the heat transfer assemblies are monitored to detect if anarea inside the microtubes is being blocked by a buildup, such asfreezing moisture, causing a decrease in the hydraulic diameter of themicrotubes. In response, various embodiments will lower the amount ofcooling being applied to the flow tunnels until the frozen moisture hasbeen cleared.

Various embodiments are adapted to provide precise dermal cooling usinga relatively small, relatively light unit that produces relativelylittle noise and relatively low vibrations. Another aspect of variousembodiments is to provide precisely controlled dermal cooling byproviding a cooled gas maintained at temperatures just above freezing toprevent cellular damage caused when cells are exposed to below freezingtemperatures.

BRIEF DESCRIPTION OF THE DRAWINGS

A more complete understanding of the methods and systems of the presentinvention may be obtained by reference to the following DetailedDescription when taken in conjunction with the accompanying Drawingswherein:

FIG. 1 is a schematic of an air cooling system in accordance with anembodiment of the present invention;

FIG. 2 is a diagram of an illustrative embodiment of the system of FIG.1;

FIG. 3 is a rear view of FIG. 2;

FIG. 4 is a side view of FIG. 2, having a side panel removed;

FIG. 5 is an exploded view of a cooling device;

FIG. 6 is an exploded view of a chamber;

FIG. 7 is an exploded view of a heat transfer assembly;

FIG. 8 is a cross-sectional view of an flow tunnel having a plurality ofmicrotubes;

FIG. 9 is a cross-sectional view of an intake silencer; and

FIG. 10 is a diagram of a condensate trap.

DETAILED DESCRIPTION OF THE DRAWINGS

When a temperature of a patient's skin is lowered, a topical anestheticeffect may be experienced resulting in less pain experienced by thepatient during many typical dermatological procedures. The anestheticeffects may become noticeable on skin that has been cooled to atemperature of about 20° C. or less. In addition to the anestheticaspects, cooling a skin surface may also minimize peripheral skin damageduring dermatological procedures, such as, for example, laser skintreatments.

A typical non-cooled skin temperature is about 32° C. If the skintemperature can be reduced quickly to about 20° C., the topicalanesthetic effect noted above can be induced quickly and thedermatological procedure performed more rapidly, thereby permitting morepatients to be treated in a given period of time. Use of gas to cool askin surface may avoid problems such as distortion of laser light beingapplied to the patient's skin and excess water being applied to thepatient and adjacent areas. During dermal application involving the useof lasers, the laser may be utilized to heat collagen underneath theskin in order to stimulate the formation of new collagen or to burn thepigment of dead follicles. When a dermal coolant lowers the temperatureof the skin too much, the efficacy of the laser may be diminished bycooling too deep into the dermis.

FIG. 1 shows a system 100 which may be used to provide cooling fordermatological applications, such as, for example, laser treatments,contour surfacing, hair removal, and other applications where coolingmay be desirable. The system 100 may also be used in other medicalapplications, such as, for example, treating patients suffering fromhypothermia. The system 100 has a cooling engine 102 for removing heatfrom a gaseous medium flowing therethrough. The gaseous medium beingcooled may include a gas, such as an inert gas, a mixture of gases, suchas air or ambient air, a gas containing moisture, such as humidity, avapor, or any other medium having gas-like properties. The terms “air,”“airflow,” or any combination of words related to the term air, as usedherein, should be broadly interpreted as referring to any gaseous mediumhaving gas-like properties, and is not used and/or presented herein aslimited to ambient air or atmospheric air.

In various embodiments, the cooling engine 102 includes one, some, ornone of the following: one or more Peltier elements, one or more heatsinks, and one or more cooling fans. The cooling engine 102 receives agaseous medium from an air mover 114. The term air mover as used hereinis being used in a generic sense to refer to any device capable ofcreating a pressure differential, such as, for example, but not by wayof limitation, a blower, a fan, a vacuum, a turbine, or any other devicecapable of causing a volume of gas to move. In the embodiment shown, theair mover 114 is disposed before the cooling engine 102 and directs thegaseous medium therethrough by creating a positive pressure at anentrance or inlet of the cooling engine 102. However, in someembodiments, the air mover 114 is disposed after the cooling engine 102and directs the gaseous medium therethrough by creating a negativepressure at an exit or outlet of the cooling engine 102.

After being cooled by the cooling engine 102, the cooled gas then flowsto a hand tool 104 having an output for supplying the cooled gas to askin surface. The cooling engine 102 may be connected to a controller108. In some embodiments, a user interface 112, including a displayand/or an input, is connected to the controller 108. The air mover 114receives the gaseous medium from an input chamber 116 which, in someembodiments, has a filter 120 for filtering the gas as it enters and/orleaves the input chamber 116. In some embodiments, the filter 120 mayinclude a noise filter or silencer for dampening noise. The coolingengine 102 may also be in fluid communication with a reservoir 136 forcollection of water resulting from the cooling of the air passingtherethrough. The cooling engine 102 and the controller 108 and the airmover 114, among other components, may be powered by one or more powersupplies 106. In some embodiments, one power supply 106 supplies powerto all the components of the system 100. In various embodiments, aplurality of power supplies 106 supply power to various components ofthe system.

Referring now to the hand tool 104 in more detail, cooled gas from thecooling engine 102 is outputted at the gas output of the hand tool 104and applied to the patient's skin. In some embodiments, a vacuum 118 maybe utilized to reduce the amount of debris resulting from adermatological procedure. In some embodiments, the hand tool 104 mayinclude a skin temperature sensor 148 and/or a skin proximity sensor150. The skin temperature sensor 148 may measure the temperature of theskin area being cooled and send the information to the controller 108.In some embodiments, the information is used to adjust the temperatureof the cooled gas being provided, for example, in a feedback loop. Insome embodiments, the information is displayed on a user-readabledisplay. The system 100 may also include a vacuum 118 interoperablyconnected to the hand tool 104 for removing the gaseous medium provided,ambient air disposed near the cooled area, and any debris on or near thearea. In some embodiments, the input chamber 116 and the filter 120 maybe used in conjunction with the vacuum 118. Additionally, a wastecanister 134 may also be used to collect the debris from the hand tool104, for example, from a patient's skin during a micro-dermabrasion orlaser peel procedure. In some embodiments, a reduced amount of energy isconsumed when the cooled gaseous medium is reclaimed after delivery tothe patient.

The hand tool 104 may also be adapted to include a coolant output ormister 138 to apply water or other coolant substance (e.g., a liquid orgel) to the skin of the patient. The coolant output 138 may beinteroperably connected to a valve to control the amount of coolantapplied via the coolant output to the skin of the patient. The coolantmay be supplied by a pump 142, for example a water pump. The amount ofcoolant applied to a patient may be controlled by the controller 108 ormay operate independent of the controller 108, for example by a valvehaving user input controls. In some embodiments, the pump 142 may not beneeded if the force supplied by the air mover 114 is great enough totransport water to a skin surface in addition to the cooled gaseousmedium supplied. In various embodiments, the pump 142 may utilize theliquid from the reservoir 136 as the coolant substance supplied to themister 138. In some embodiments, a UV light or other viricide orbactericide treatment is used to sanitize the liquid in the reservoir136.

Still referring to various embodiments related to the hand tool 104, acoolant output may be used to provide additional topical anestheticeffect via, for example, evaporative cooling. In some embodiments, askin temperature sensor is utilized to provide feedback to the user andto the controller 108. In some embodiments, a proximity sensor mayprovide feedback to the user so that the hand tool 104 is positioned bythe user at an optimal distance from the skin of the patient. In someembodiments, the hand tool 104 may also include a laser used for laserdermatological applications or other tools used in dermatologicalapplications. In other embodiments, the hand tool 104 may includeattachment points adapted to connect a laser thereto. The source of thelaser may be located at the hand tool 104, or may be remotely disposedfrom the hand tool 104 and optically connected therewith.

Referring now to the system 100 in general. The system 100 is adapted toprecisely control the temperature and pressure of the gaseous mediumbeing supplied to the hand tool 104. In various embodiments, a outputsensor 126 is disposed between the cooling engine 102 and the hand tool104 to monitor the temperature and pressure of the gaseous medium aftercooling. The output sensor 126 may be located near the cooling engine102 and adapted to provide temperature and pressure information for usein determining the temperature of the gaseous medium at a remotelocation, such as at the exit of the hand tool 104. In some embodiments,an algorithm is used based on the characteristics of a delivery hoseused to deliver the gaseous medium to the hand tool 104, such as, forexample, length of the delivery hose and insulating capabilities of thehose, such as, the thermal conductivity of the material used to make thehose. As will be explained further below, the delta-T (T₂-T₁) betweenthe exit of the cooling engine 102 and the exit of the hand tool 104 canbe determined based on one or more of the following observableconditions: the temperature of the gas flowing in the hose, the pressureof the gas flowing in the hose, the ambient temperature outside of thehose, the insulating properties of the hose, and the length of the hose.For example, the input chamber 116 may include a temperature sensor tomeasure the temperature of the ambient air for use in theabove-mentioned calculations.

In the system 100, the controller 108 may be used to vary the flow rateof the gaseous medium flowing through the cooling engine 102. Thecontroller 108 may also precisely control the temperature to which thecooling engine 102 cools the gaseous medium flowing therethrough. Invarious embodiments, the system 100 is adapted to run on a variety ofinputted AC or DC voltage ranges, for example, off a DC power sourceranging from, on the order of 150-340 V_(dc) or AC power source rangingfrom, on the order of 95-250 V_(ac). In some embodiments, thetemperature to which the gaseous medium is cooled is varied by varyingthe amount of power supplied to the Peltier devices (or TEC arrays) bythe power supply 106. The power supply 106 driving the TEC array's mayhave variable output of between, for example, on the order of 5-135V_(dc) which can be varied by the controller using, for example, a PulseWidth Modulation (PWM) signal. By varying the output of the power supply106, the power to the TEC arrays can be modulated to achieve precisetemperature control. Varying the output also allows the HTA module touse a minimum amount of input power while providing optimal control,lowering the overall input power required by lowering the drive voltage.

In some embodiments, the cooling engine 102 may be a solid-state heatpump, referred to above as a Peltier device or a TEC device. When thecooling engine 102 is operated in a cooling mode, the direction ofelectrical current applied to one or more Peltier elements of thecooling engine 102 is chosen so as to cause a side of the one or morePeltier devices in thermal contact with one or more flow tunnels toremove heat therefrom. The one or more flow tunnels may have a gaseousmedium flowing therethrough and in thermal contact therewith. When theone or more Peltier devices remove heat from the one or more flowtunnels, heat is thereby removed from the gaseous medium flowingtherethrough and the gaseous medium is cooled thereby. When inoperation, heat removed by the one or more Peltier elements must berejected to the ambient environment. As will be explained in greaterdetail below, in various embodiments, one or more heat sinks thermallycoupled to the one or more Peltier devices and operating in conjunctionwith one or more cooling fans facilitate rejection of the removed heatto the ambient environment. As will be explained in more detail below,the system may also include a defrost cycle. In various embodiments, thesystem 100 monitors various conditions to detect whether a hydraulicdiameter of the flow tunnels has been reduced by, for example, frozenmoisture from the gaseous medium passing therethrough. In someembodiments, the gaseous medium to be cooled is drawn from the ambientare around the system 100. When the TEC arrays actively cool, oractively remove heat from, the flow tunnels, moisture, usually in theform of water, may be deposited on an inside portion of the flowchannels. When the TEC arrays actively cool the flow tunnels to atemperature below a freezing point of the moisture containedtherewithin, the moisture may freeze, or solidify, and deposit onto theinside of the flow tunnels thereby reducing a hydraulic diameterthereof. The water, When it is determined that the hydraulic diameterhas decreased by a predetermined amount, the system may decrease theamount of power supplied to at least one of the one or more Peltierdevices until the frozen moisture has been reduced and the hydraulicdiameter returned to at or near a normal operating size. In someembodiments, the electric current supplied to at least one of the one ormore Peltier devices may be reversed thereby actively heating the atleast one of the one or more Peltier devices.

For the defrost cycle, the air velocity coming out of the device ismonitored by measuring the pressure. In various embodiments, when thecontrol unit is turned on, the control unit will do an auto-calibrationof the pressure. The expected pressure at that particular altitude willbe compared to factory set parameters. At each power-up thereafter, thecontrol unit will run a calibration check to make sure everything isoperating correctly.

As noted above, the cooling engine 102 includes an output sensor 126.The controller 108 may use information, such as temperature andpressure, monitored by the output sensor 126 along with otherinformation in an algorithm to make determinations, such as, forexample, how much power should be supplied by the power supply 106 todrive the cooling engine 102 to reach a particular temperature in aparticular amount of time. In some embodiments, feed back from theoutput sensor 126 is used to adaptively adjust the amount of powerapplied to the cooling engine 102 to reach a desired temperature in adesired amount of time and also to maintain the desired temperature.

In some embodiments, the system 100 may also be used to treathypothermia by heating the patient's skin, for example, to 33-35° C. Inorder to heat a gaseous medium passing through the cooling engine 102,current applied to the one or more Peltier elements of the coolingengine 102 is reversed relative to that applied when the cooling engine102 is used to cool the gaseous medium. In some embodiments, an airblanket or the like (not shown) may be used in place of the hand tool104 to apply the warmed gaseous medium to the patient. The air blanketmay be used to circulate the warm gas around one or more portions of thepatient's body. When used as a heating device, recirculation of heatedgas from the air blanket back to the cooling engine 102 may be employedas dictated by various design considerations.

Referring again to the system 100 in general, various embodiments areadapted to provide a cooled gaseous medium at a temperature just abovefreezing in order to only cool a top layer of a skin surface, such asthe thin microns of the subdermis to numb the nerve fibers proximatelydisposed there. Various embodiments are adapted to provide the cooledgaseous medium without the use of a compressor. In various embodiments,the system 100 is adapted to provide the cooled gaseous medium to aremote location, for example a remotely disposed skin surface, atbetween on the order of 0 and 3° C. In some embodiments, a solid-statecooler is provided capable of accurately providing a cooled gaseousmedium at a flow velocity of over 1000 liters per minute. In variousembodiments, a standby mode is utilized where the temperature of thegaseous medium is provided at a constant temperature, for example,around, on the order of, 10° C. From the standby mode, upon activation,various embodiments may be capable of providing a cooled gaseous mediumto a remote location at between, on the order of, 0 and 3° C. within 90seconds and in some embodiments, as little as 60 seconds. Variousembodiments are adapted to provide continuous therapy for a full day oftreatment without needing to be defrosted. In some embodiments, anautomatic internal defroster is provided that automatically defrosts tokeep the device from freezing up.

Referring now to FIG. 2, a system 200 is shown according to anembodiment. The system 200 has a control unit 202 with a delivery hose204 connected thereto. The control unit 202 cools a gaseous medium thatthen flows through the delivery hose 204 to an exit 206. The exit 206may be connected to a hand unit (not shown) for assisting a user incontrolling and directing the airflow out of the exit 206. In someembodiments, a shut-off valve may be located along the delivery hose204, wherein the shut-off valve is adapted to allow a user todiscontinue the airflow out of the exit 206 without having to return tothe control unit 202. In some embodiments, the shut-off valve may bemonitored and, for example, the gaseous medium could be internallycirculated, for example, by opening a valve so the gaseous medium mayflow from the bottom chamber to the top chamber.

Various embodiments may use a plurality of different hose sizes andtypes to transport the cooled gaseous medium to the skin surface.Various hoses may be more rigid, while other hoses may be more lightweight or more flexible. In various embodiments, a hand piece (notshown) may be attached to the end of the delivery hose 204 to facilitateadministration of the cooled air. The hand piece may be adapted toaccommodate a plurality of different nozzles that can be attached to thedelivery hose 204 or to the hand piece, such as a nozzle for delicatecooling, for example, around a facial region, or a nozzle for large-areacooling, such as on a back region. In various embodiments, the flow ratecan be variably controlled by one, both, or neither of the controller orthe nozzle, for example, so that the airflow can be turned down whilecooling a facial region and turned up while cooling a back region.Various embodiments may have indicators for alerting the user that theairflow through the delivery hose 204 may be blocked, for example, by akink in the delivery hose 204.

The control unit 202 also has a user interface 208 where a user maychange various settings such as the temperature and/or the flow rate ofthe gaseous medium being provided. In the embodiment shown, the controlunit 202 has wheels 210 disposed on a lower portion thereof forfacilitating movement of the control unit 202. It can also be seen thatthe control unit may have vent slats 212 disposed on one or moresurfaces thereof. In the embodiment shown, the vent slats 212 arelocated on a side panel of the control unit 202. As will be explained inmore detail below, the vent slats 212 may allow ambient air to passtherethrough.

Referring now to FIG. 3, a rear view of a control unit 302 is shown.Wheels 310 can be seen disposed on a lower portion of the control unit302. Air vents 312 can also be seen disposed on various portions of arear panel of the control unit 302. A communication port 314 can also beseen. In some embodiments, the communication port 314 may allow thecontrol unit 302 to send and/or receive signals from other electronicdevices. The communication port 314 may be a USB port, a serial port, anEthernet port, an RS485 ports, an RS232, an antenna for sending andreceiving wireless signals, or any other input/output port for sendingand/or receiving signals. A transport handle 316 disposed on the rearpanel of the control unit 302 can be seen. In the embodiment shown, thetransport handle 316 is disposed on an upper portion of the rear panel,but the transport handle 316 may be located anywhere on the control unit302. A power switch 318 for turning the control unit 302 on and off canbe seen. The power switch 318 may be located anywhere on the controlunit, but in the embodiment shown, it is disposed on an upper portion ofthe rear panel. The power switch 318 may include a circuit breaker suchas, for example, a ground fault circuit interrupter. A power-entrymodule 320 is also shown disposed on a rear panel of the control unit302. An intake opening 322 can also be seen. The intake opening 322 mayalso have a filter 324, such as, for example, a HEPA filter. In someembodiments, the intake opening 322 is where all, some, or none of thegaseous medium to be cooled by the control unit 302 enters. The filter324 may be utilized to ensure the gaseous medium to be cooled isrelatively clean and relatively free of particulate or other debris. Asill be explained further below, the intake opening 322 may be in flowcommunication with a noise filter. In the embodiment shown, the intakeopening 322 is located near a lower portion of a rear portion of thecontrol unit 302, however the intake opening 322 may be located anywhereon the control unit 302. In some embodiments, the intake opening 322also includes one or more connectors to connect to a supply hose thatsupplies a gas or other medium.

Referring now to FIG. 4, an cooling system 400 is shown where a controlunit 402 is shown with a side panel removed for descriptive purposes. Adelivery hose 404 is attached to a hose interface 403. The hoseinterface 403 may be a quick connect type interface, may have screwraces, or may include any other way of connecting the delivery hose 404to the control unit 402. A drip pan 426 can be seen attached to anunderneath portion of the air cooler system 400. The drip pan 426 may beused to catch condensate resulting from the cooling done by the coolingengine. One characteristic of gases and moisture therewithin is that agas at a higher temperature may hold a larger quantity of moisturetherewithin. As the gas is cooled from a first higher temperature to asecond lower temperature, moisture suspended therewithin will no longerremain suspended therewithin and will begin condensating. An increasingamount of moisture will condensate as the temperature of the gas islowered. The drip pan 426, disposed on a lower portion of the controlunit 402, is adapted to capture the moisture as condensation occurs as aresult of the cooling of the gaseous medium. In some embodiments, thedrip pan 426 is a removable tray for ease of emptying. In someembodiments, the drip pan 426 includes a drain hose for draining thecondensate therefrom.

As previously mentioned, the control unit 402 may utilize thermoelectriccooler (TEC) arrays to cool a gaseous medium. A power source 428disposed within the control unit 402 is adapted to power, among otherthings, the controller, the TEC arrays, and various fans and/or pumps.In some embodiments, a plurality of power sources may be utilized topower various electrical components. In some embodiments, one or morepower supplies are used to power the TEC arrays and do not power anyother components. In some embodiments, a fan assembly 430 may beincluded to cool the power source 428. An air mover 432, such as ablower, is disposed within control unit 402 for blowing a gaseous mediumpast the heat transfer assembly (HTA) modules 442 and through thedelivery hose 404. A fan 434 may also be included to cool the air mover432. In some embodiments, the temperature of the air mover 432 ismonitored and the fan 434 is used to modulate the temperature of the airmover 432. A table top 436 may be disposed above an upper portion of thecontrol unit 402. A support 438 may be utilized to support the weight ofone or more objects placed on the table top 436. Below the HTA module442, a bottom chamber 440 can be seen. Sensors 405 and 407 can be seendisposed above and below the HTA module 442. In some embodiments, thesensors 405 and 407 may monitor temperatures and pressures of thegaseous medium being cooled by the HTA module 442.

Referring now to FIG. 5, an exploded view of a portion of a control unit502 is shown. The gaseous medium from an air mover, such as a blower(not shown), enters a top chamber 544. The gaseous medium passes througha plurality of HTA modules 542 to be cooled and down to a bottom chamber540. The cooled gaseous medium then proceeds to the delivery hose 504for use in a dermatological applications. A plurality of fans 546,exploded for descriptive purposes, may be disposed on one, both, orneither side of the HTA modules 542 to provide a flow of ambient airthereacross to remove heat therefrom. In some embodiments, the pluralityof fans 546 may be disposed in a push-pull relationship relative to theHTA modules 542 in order to provide an increased flow of ambient airthereacross to remove heat therefrom.

Referring now to FIG. 6, an exploded view of a top portion of a controlunit 602 is shown. The gaseous medium enters the air mover, such as ablower, 632 and is blown into the top chamber 644. As previouslymentioned, in some embodiments, the air mover 632 may create either apositive pressure of a negative pressure relative to the HTA modules642. As can be seen from the embodiment shown, the top chamber 644expands from a narrow entrance opening to a large exit opening. Having alarge exit opening creates an area of low pressure relative to theentrance opening. This low pressure area above the HTA modules 642 helpscreate an environment conducive to turbulent flow. By expanding the areaof the top chamber 644, a back-pressure against the air mover 632 can beminimized The gaseous medium then flows into the flow tunnels 648 of theHTA modules 642.

There is an upper chamber 644, such as an intake manifold, over aplurality of flow tunnels 648. The top chamber 644 is monitored to lookat the airflow based on the characteristics of the air mover 632. Thecontrol unit 602 may utilize an air mover 632, such as one or more of ablower, a pump, a vacuum, a positive displacement pump, a centrifugalpump, a turbine-style magnetically coupled pump, or any other device forcreating a pressure differential.

Referring now to FIG. 7, an exploded view of the HTA modules 742 isshown. The gaseous medium passing through the flow tunnels 748 iscooled. A TEC array 750 in thermal contact with the flow tunnels 748removes heat therefrom. A TEC array 750 may be disposed on either sideof the flow tunnels 748. Heat sinks 752 are disposed on an outside ofthe TEC arrays 750 to remove heat therefrom. The flow tunnels 748 haveinlets and outlets. To cool the gaseous medium flowing therethrough,various embodiments utilize flow tunnels 748 thermally coupled to one ormore banks of TEC arrays 750. In the embodiment shown, the flow tunnels748 are sandwiched between a plurality of TEC arrays 750. As will beexplained in more detail below, in some embodiments, the flow tunnels748 are formed having low-profile extrusions, or microtubes, runningtherethrough. In some embodiments, the microtubes have a plurality ofmicrochannels running along an inside surface thereof.

Referring now to FIG. 8, a cross-sectional view of an flow tunnel 848can be seen. The flow tunnel 848 is formed from a heat conductivematerial adapted to transfer heat between a plurality of TEC arrays (notshown) and a gaseous medium flowing through the flow tunnels 848. Theflow tunnels 848 also have a plurality of microtubes 856 therein tofacilitate airflow therethrough. As can be seen from the embodimentshown, the microtubes 856 are adapted to have microchannels 854 runningalong an interior surface thereof thereby increasing the surface area ofthe interior of the microtubes 856. The microchannels 854 may be formedfrom surface enhancers 853 extending from the interior surface of themicrotubes 856. The surface enhancers 853 provide an increased area ofcontact between the gaseous medium flowing thereby thus increasing thethermal conduction therebetween. One way of calculating the hydraulicdiameter, or the flow area, of a microtube 856 is to measure thediameter of the area of the microtube 856 including the depth of themicrochannels 854 and subtract the area of the surface enhancers 853.Another way of calculating the hydraulic diameter of a microtube 856 isto measure the area of the microtube excluding the depth of themicrochannels 854 and add the of the microchannels 854. The two abovementioned calculations should result in a same hydraulic diameter, thatis the cross-sectional area available for the gaseous medium to flowtherethrough.

The surface enhancers 853 may also increase the Reynolds number of theflow path. In fluid mechanics, an increased Reynolds number isindicative of relatively turbulent flow while a decreased Reynoldsnumber is indicative of a relatively laminar flow. At high Reynoldsnumbers, the turbulent flow may include competing inertial forces, whichmay produce random eddies, vortices, and other flow fluctuations. Insome embodiments, it may be desirable to have the surface enhancers 853adapted to increase the Reynolds number and thus create a turbulent flowprofile within the microtubes 856. The increased turbulence may increasethe amount of heat exchanged between the flow tunnels 848 and thegaseous medium flowing therethrough.

In some embodiments, an upper edge of the microtubes 856, for example,an inlet of the microtube 856, may be chamfered, or beveled or otherwisemachined, to create a conically shaped opening at the inlet thereof. Insome embodiments, a plurality of microchannels 854 may be disposedaround an interior surface of the microtubes 856 to form a, for example,starburst-like shape. Various embodiments utilizing microchannels 854and surface enhancers 853, may increase the contact area between theflow tunnels 848 and the gaseous medium flowing therein by as much as 30to 40%. In some embodiments, the flow tunnels 848 are made of athermally conductive material, such as, for example, aluminum, but theflow tunnels 848 can be made of any material that will allow thermalconductivity between the flow tunnels 848 and the gaseous medium flowingtherethrough.

Referring now to FIG. 9, a cross-section of an embodiment of an intakesilencer 922 is shown. The ability to reduce noise caused by airflow maybe desirable in many applications, for example, where the environmentthe control unit is being operated in is relatively quite. In someembodiments, acoustic baffles may be used to minimize audible noisescaused by the control unit, for example, in the 15 dB range caused by,for example, the howling or whistling effects of an air mover. Theintake silencer 922 may have a single intake port that then has theairflow separated into a plurality of flow paths through a plurality oftubes. The plurality of tubes may then have a plurality of perforationsallowing the gaseous medium to exit through the plurality ofperforations. Additionally, a filler, such as polyester, may be disposedbetween the plurality of tubes and the exit port. The exit port may alsohave a plurality of perforations therein to allow the air to passtherethrough.

Referring now to FIG. 10, a side view of a cross-section of a bottomchamber 1040 can be seen. After the gaseous medium has been cooled bythe HTA modules (not shown), the gaseous medium flows to the bottomchamber 1040, as shown. The gaseous medium flows through the bottomchamber 1040 and out the hose interface 1003 to the delivery hose 1004for use in a dermal application. To minimize the water content of thecooled gaseous medium delivered to the patient, a condensate trap 1062is provided in the bottom chamber 1040. For example, in someembodiments, the condensate trap 1062 is placed at a 45° angle relativeto the flow path. As the gaseous medium flows across the surface of thecondensate trap 1062, moisture in the gaseous medium condenses on thesurface of the condensate trap 1062. Similarly, any water particles orother moisture will hit the condensate trap 1062 and flow downtherefrom.

In some embodiments, the amount of condensation collecting in the drippan of the bottom chamber 1040 may be monitored. In some embodiments, alevel monitor monitors the amount of condensation, for example the waterlevel inside the drip pan. In some embodiments, the conditions at whichthe control unit is being run are monitored and the amount ofcondensation is predicted. For example, the humidity of the gaseousmedium being cooled and the amount of cooling being done may be used asan indicator of the amount of condensation that will accumulate. In someembodiments, an alarm may alert a user that the drip pan needs to beemptied. In some embodiments, a drain may be attached to the drip pan toallow drainage of the condensate. In some embodiments, a valve, such asa solenoid valve, may be utilized to allow the drip pan to be drainedautomatically.

The previous description is of a preferred embodiment for implementingthe invention, and the scope of the invention should not necessarily belimited by this description. The scope of the present invention isinstead defined by the following claims.

1. A system adapted to thermally affect a gaseous medium fordermatological applications, the system comprising: a plurality of flowtunnels having inlets and outlets; an air mover adapted to impartairflow to a gaseous medium through the plurality of flow tunnels; aplurality of thermoelectric coolers thermally coupled to the pluralityof flow tunnels and adapted to actively remove heat therefrom to coolthe gaseous medium flowing therethrough; a sensor adapted to monitor atleast one indicator relative to the flow of the gaseous medium throughthe plurality of flow tunnels and send a signal if a hydraulic diameterof at least one of the plurality of flow tunnels decreases; and whereinthe amount of heat being actively removed by at least one of theplurality of thermoelectric coolers from at least one of the pluralityof flow tunnels is reduced in response to the signal.
 2. The system ofclaim 1 wherein the indicator is a pressure of the gaseous medium. 3.The system of claim 1 wherein the indicator is a flow rate of thegaseous medium.
 4. The system of claim 1 and further comprising: adelivery hose having a thermal conductivity and a length adapted todeliver the gaseous medium to a remotely disposed location.
 5. Thesystem of claim 4 wherein a temperature of the gaseous medium at theremotely disposed location is calculated based on the thermalconductivity and the length of the delivery hose and a temperature ofthe gaseous material entering the delivery hose.
 6. A system adapted tothermally affect a gaseous medium for dermatological applications, thesystem comprising: a plurality of flow tunnels having inlets andoutlets; a delivery hose having thermal conductivity characteristics andhaving an input and an output, the input adapted to be connected to theoutlets of the flow tunnels; an air mover adapted to impart airflow to agaseous medium through both the plurality of flow tunnels and thedelivery hose connected thereto; a plurality of thermoelectric coolersthermally coupled to the plurality of flow tunnels and adapted toactively remove heat therefrom to cool the gaseous medium flowingtherethrough to a predetermined temperature; and wherein thepredetermined temperature is calculated based on the thermalconductivity characteristics of the delivery hose and a desiredtemperature of the gaseous medium at the output.
 7. The system of claim6 and further comprising: a sensor to monitor the pressure of thegaseous medium.
 8. The system of claim 6 wherein the air mover isadapted to create a pressure differential to impart airflow through theflow tunnels.
 9. The system of claim 8 wherein the gaseous medium isdrawn from ambient air containing moisture and the system includes amonitor for measuring the pressure differential.
 10. The system of claim9 wherein the monitored pressure differential is adapted to indicate areduction in hydraulic diameter of at least one of the plurality of theflow tunnels.
 11. The system of claim 10 wherein the reduction inhydraulic diameter is the result of the moisture freezing in at leastone of the plurality of flow tunnels.
 12. The system of claim 11 whereinthe system is adapted to reduce the active removal of heat by thethermoelectric coolers in response to the monitored indication of frozenmoisture in the flow tunnels.